Design and Analysis of Aircraft Wing Angles Estmation Using Python Tool

The wing is a superstructure that can fly thanks to an airfoil profile that generates lift from the forward motion of the vehicle. There are two ends of the cantilever structure on fixed-wing aircraft: one is let free and the other is fixed. In this article, CREO is used to simulate the precise structure of an Aeroplan wing with a winglet. Once the wing structure has been analyzed, pressure analysis of the wing's structure is carried out. An ANSYS model is used to determine the winglet's safety factor using a restricted component method with the help of ANSYS. There must be an exhaustion damage aggregation modeling, constant abundance of S-N (stress life) information for various pressure proportions, and the stress history of the neighborhood at the pressure focus in order for the safety factor to be effective. The aircraft wing with winglets (450 and 250 points) is examined in this theory. The winglet points (450 and 250) are subjected to a static and fatigue research in order to determine the load and life of the winglet due to the applied weight loading. At 250winglet is performing well and getting expected results. This entire work is estimated in python tool 3.6.8 version.